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Design and Testing of Pneumatic Systems for Measuring Low Pressures in Hypersonic Wind Tunnels.

机译：高超声速风洞低压力气动系统的设计与试验。

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作者
Wagner, M. J.; Dale, G. A.;
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年度 1985
页码 1-41
总页数 41
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Hypersonic wind tunnels; Test and evaluation; Computer programs; Cost effectiveness; High temperature; Transducers; Viscous flow; Orifices; Time lag theory;

机译：高超声速风洞;测试与评估;计算机程序;成本效益;高温;传感器;粘性流;孔;时滞理论;

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Design and Testing of Pneumatic Systems for Measuring Low Pressures in Hypersonic Wind Tunnels.

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